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100   $a20110225j199708    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign of launch vehicle flight control augmentors and resulting flight stability and control (center director's discretionary fund project 93-05, part III) /$fC. Barret
210  1$aMSFC, Alabama :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$dAugust 1997.
215   $a1 online resource (xii, 63 pages) $cillustrations
225 1 $aNASA technical paper ;$v3704
300   $aTitle from title screen (viewed on April 28, 2016).
300   $a"August 1997."
300   $a"Performing organization: George C. Marshall Space Flight Center, Marshall Space Flight Center, Alabama"--Report documentation page.
320   $aIncludes bibliographical references (pages 62-63).
517   $aDesign of launch vehicle flight control augmentors and resulting flight stability and control 
606   $aDesign analysis$2nasat
606   $aLaunch vehicles$2nasat
606   $aAugmentation$2nasat
606   $aFlight control$2nasat
606   $aStability tests$2nasat
615  7$aDesign analysis.
615  7$aLaunch vehicles.
615  7$aAugmentation.
615  7$aFlight control.
615  7$aStability tests.
700   $aBarret$b C.$01396940
712 02$aGeorge C. Marshall Space Flight Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bSSM
801  1$bSSM
801  2$bGPO
906   $aBOOK
912   $a9910707158003321
996   $aDesign of launch vehicle flight control augmentors and resulting flight stability and control (center director's discretionary fund project 93-05, part III)$93457911
997   $aUNINA